Effect of stabilizer location upon pitching and yawing moments in spins as shown by tests with the spinning balance (1933)
NASA Technical Reports Server (NTRS) · leaf 17
.08 .08r o Normal o Normal .04 .04- + Forward + Forward Stabilizer Stabilizer a Aftf 1 a Aft location location … 40 50 60 70 40 50 60 70 Angle of attack at center of gravity, degrees Angle of attack at center of gravity, degrees Figure 11.-Pitching-moment coefficients due to Figure 12.-Pitching-moment coefficients due to a stabilizer and elevator. Sideslip at stabilizer and elevator. Sideslip at e.g. ^ eg-.…
NASA Technical Reports Server (NTRS)
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